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5059 Aluminum vs. SAE-AISI 4340M Steel

5059 aluminum belongs to the aluminum alloys classification, while SAE-AISI 4340M steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is 5059 aluminum and the bottom bar is SAE-AISI 4340M steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 11 to 25
6.0
Fatigue Strength, MPa 170 to 240
690
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
72
Shear Strength, MPa 220 to 250
1360
Tensile Strength: Ultimate (UTS), MPa 350 to 410
2340
Tensile Strength: Yield (Proof), MPa 170 to 300
1240

Thermal Properties

Latent Heat of Fusion, J/g 390
280
Maximum Temperature: Mechanical, °C 210
430
Melting Completion (Liquidus), °C 650
1440
Melting Onset (Solidus), °C 510
1400
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 110
38
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 95
9.1

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.9
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.1
1.9
Embodied Energy, MJ/kg 160
26
Embodied Water, L/kg 1160
55

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 42 to 75
120
Resilience: Unit (Modulus of Resilience), kJ/m3 220 to 650
4120
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 36 to 42
84
Strength to Weight: Bending, points 41 to 45
51
Thermal Diffusivity, mm2/s 44
10
Thermal Shock Resistance, points 16 to 18
70

Alloy Composition

Aluminum (Al), % 89.9 to 94
0
Carbon (C), % 0
0.38 to 0.43
Chromium (Cr), % 0 to 0.25
0.7 to 1.0
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 0 to 0.5
93.3 to 94.8
Magnesium (Mg), % 5.0 to 6.0
0
Manganese (Mn), % 0.6 to 1.2
0.65 to 0.9
Molybdenum (Mo), % 0
0.35 to 0.45
Nickel (Ni), % 0
1.7 to 2.0
Phosphorus (P), % 0
0 to 0.012
Silicon (Si), % 0 to 0.45
1.5 to 1.8
Sulfur (S), % 0
0 to 0.012
Titanium (Ti), % 0 to 0.2
0
Vanadium (V), % 0
0.050 to 0.1
Zinc (Zn), % 0.4 to 0.9
0
Zirconium (Zr), % 0.050 to 0.25
0
Residuals, % 0 to 0.15
0